Specifications - USCG C37B Purchase.pdf

U. S. COAST GUARD

Long Range Command and Control Aircraft

C-37B Aircraft Requirements

Delivery Order Solicitation #: TBD

Gulfstream Serial #: TBD

Statement of Work - ATTACHMENT 1

USCG C-37B SOW (Spec) Attachment 1

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Table of Contents

Introduction BUYER-Approved Documents Terminology Roles and Responsibilities

GULFSTREAM Government Program Manager

Customer Delivery Executive

Aircraft Manager

BUYER Representatives

Viewing Rights

Work Change Requests (WCRs)

Procedures

Aircraft Service Changes

Customer Bulletins, Alert Customer Bulletins and Maintenance and Operations Letters

Inspection Requirements

1000 Shop Group Leaders

1010 Quality Assurance Inspection

1020 Aircraft Preservation

1030 Weight and Balance

1040 BUYER Support Data with Maintenance Handbooks

1060 GULFSTREAM Equipment Removal and Functional Checks Interior

General Interior

2000 Title 14 CFR Part 91 Compliance Requirements

2020 Covering Materials and Finish

2030 Floor Covering

2040 Material Soil and Stain Prevention Treatment

2050 Underfloor Access

2060 Soundproofing

2065 Corrosion Prevention Treatment

Cabin Headliners and Passenger Service Units

2070 Headliner and Passenger Service Units with Handrails

2080 Cabin Lighting

Cockpit Area

2100 Cockpit Area Furnishings and Finish—Gray

2110 Cockpit Panel Modifications

2120 Cockpit Area Electrical

Main Entryway and Vestibule Areas

2130 Main Entry Door

2140 Vestibule Area

2170 Entranceway Decorative Treatment

2180 Jeppesen Manual Storage

2190 Avionics Compartments

2200 Vestibule Acoustical Closeout

2220 Forward Closets

2230 Forward Crew Refreshment Compartment

2270 Forward Crew Lavatory

Cabin Seating

2280 Single Passenger Seats

Cabin Tables and Ledges

2320 Console Tables

2341 Communication System Operator’s—(CSO) Station

2381 Cabin Ledges

Cabin Windows

2391 Cabin Window Shades

2400 Window Panels

Cabin Bulkheads and Doors

2420 Forward Cabin Bulkheads with Hinged Door

2431 Mid-Cabin Bulkheads with Pocketing Doors

2445 Mid-Cabin Closets

2450 Aft Cabin Bulkhead(s)

2456 Aft Cabin Curtain

Aft Galley/Galley Annex Area

2464 Aft Galley/Galley Annex—Open Cabin

Aft Lavatory Area

2480 Aft Lavatory Bulkheads and Door

2491 Aft Lavatory—Side Facing with Opposite Vanity

2501 Aft Closet(s)/Storage Compartment(s)

Baggage Compartment

2510 Baggage Compartment Bulkhead and Door

2530 Baggage Compartment Emergency and Loose Equipment

2540 Emergency Equipment

2550 Loose Equipment Interior Systems

2560 Emergency Lighting System

2570 Crew Oxygen System

2580 Passenger Oxygen System

2590 Water and Drain System

2600 Conditioned Air Modification

2610 Cabin/Lavatory Call System and Passenger Warning Signs

2622 Passenger Audio System

2630 Cabin Stereo Equipment

2650 Cabin Video Equipment

2655 GULFSTREAM Audio/Video Distribution System

2668 SecuraPlane Camera System

2671 Airshow 4000 Passenger Flight Information System

2680 Cabin Switch Panel

2690 60/400 Hertz Power System

2700 Aisle Lights

2710 Vacuum Waste System Aft Utility Compartment

General Aft Utility Compartment

3000 Aft Utility Compartment Lighting

3010 Tow Bar Storage

3030 Maintenance Storage Box

3080 Tronair Axle Jack

3090 Battery Charger Covers Avionics

General Avionics Systems

4030 Spare Wires and Conduits Flight Communications

4000 Cockpit Audio System

4010 Radio Master System

4118 VHF Communication Modification

4119 HF Communication Modification

4125 SATCOM Direct Optelity (or Equivalent) Airborne Telephone System

4128 UHF Communication

4158 Raytheon APX-119 IFF System Mission Systems

4234 Honeywell MCS-7120 SATCOM

4235 UHF Military SATCOM System

4236 Wulfsberg Electronics C-5000 Communications Management System

4239 High Speed Data System (HSD 400)

4240 Viasat KA/KU Communication System

4241 Integrated Communications Switching Systems

4330 Maintenance Computer

4420 Automatic Dependent Surveillance– Broadcast (ADS-B) Out V2 Installation

4580 Trimble GPS 37 P(Y) Code

4582 Collins AN/ARN-153V TACAN System

4750 Securaplane PreFlite Aircraft Security System Exterior

General Exterior

5000 Exterior Paint

5030 Forward External Switch Panel

5048 Grounding Points

5060 28 Volt DC Ground Service Bus

5130 External Service Compartment Lighting/Service Door Open Warning

5221 “IRU ON”, Battery Indicator

5235 “Right-Hand Engine Cowl Open” Indicator

5260 Common Keyed Locks

5271 Engine Inlet Covers—Soft Type

5288 Engine and APU Oil

6000 Aircraft Service Changes—(ASCs)

Introduction

This document defines the installation of the avionics, electrical equipment and cabin systems, the fabrication and installation of the executive interior furnishings, and the application of exterior paint for the

United State Coast Guard referred to as the BUYER. References to GULFSTREAM throughout this document shall be understood to mean Gulfstream Aerospace Corporation. Any variations from this SOW and the current C-37B in production requires written approval from BUYER contracting officer unless said variations are due to obsolescence issues or enhancements in the production aircraft and mutually agreed upon.

BUYER-Approved Documents

This document does not address the final decor and finish treatment of the materials (e.g., woods, fabrics, leathers) that are used in completing the interior of the Aircraft. A design package, which includes a sample of the materials, shall be submitted to the BUYER for approval. GULFSTREAM will confirm projected date of Design Package availability upon assignment of Completion Outfitting Center. Upon release of initial draft, GAC will host Design Package Review with USCG team. The Completion

Package, as mutually agreed upon by the BUYER and GULFSTREAM, shall be comprised of the following documents signed by both parties:

Completion Specification

Design package (Drawing Number GC578045xxx ) – two copies

Interior styling package

• Floorplan with elevations

• Major elevations and layouts

• Berthing layout

• Seat perspective

• Table and ledge details

• Layouts for main cabin furniture

• Galley/Galley Annex layouts

• Lavatory layouts

• Closet layouts

• Baggage compartment layouts

Seat renderings

Exterior paint scheme

• Rendering

• Technical drawing

Material color board with plating

Wood sample

Carpet sample

Veneer and hardwood

Software definition document

In the event of conflicts between the contents of this document and other technical documents, drawings, layouts, etc. in the Completion Package, the contents of this document shall take precedence.

In no instance, will this document take precedence over the contract terms and conditions.

Terminology

The words “full provisions for...,” “partial provisions for...,” “wiring provisions for...,” ”space provisions for...,” “storage provisions for...,” or “Government Furnished Equipment (GFE)...,” shall have the following meanings whenever used in this document:

“Full provisions for...”

Full provisions for a specific item of equipment, assembly, or installation shall mean that all supports, brackets, tubes, fittings, electrical wiring and connectors, and hydraulic lines have been installed.

Adequate space has been allocated for the future installation of components, i.e., mission equipment without alteration to the specified equipment or the Aircraft. System functional testing and certification shall be accomplished at additional cost when the BUYER purchases the components, i.e., mission equipment. Installations of complete provisions shall be based on the information available at the time of installation and therefore do not imply the completeness of such provisions at any future date.

“Partial provisions for...”

Partial provisions for an item of equipment shall mean that the specified level of system provisions are such that additional labor/material is required to complete installation of the item. Wherever partial provisions are installed, this document shall identify the level of provisions that are to be installed.

“Wiring provisions for...”

Wiring provisions for a specific installation shall mean that only the wiring required for that installation shall be installed, capped and stowed at both ends. Installations of wiring provisions shall be based on the information available at the time of installation and therefore do not imply the completeness of such provisions at any future date.

“Space provisions for...”

Space provisions for a specific installation shall mean that the space required for that installation is unoccupied in the Aircraft. “Space provisions” does not imply that any attaching structure, brackets, bolt holes, electrical wiring and connectors, etc., shall be furnished, designed or installed, or that the installation itself shall be accomplished.

“Storage provisions for...”

Storage provisions for such items as cutlery, glassware, stemware, dishware, china, and digital video discs shall be fabricated. The storage provisions shall consist of standard partitions and racks only.

Custom size racks, partitions and dividers can be fabricated and installed by GULFSTREAM at an additional cost through a Work Change Request.

“Government Furnished Equipment (GFE)”

Government Furnished Equipment (GFE) shall mean items or components, which are to be procured and furnished to GULFSTREAM by the BUYER for use specifically identified in this document or a Work

Change Request. The BUYER shall be fully responsible for any applicable certification requirements, shipping and handling or repair costs. The BUYER must furnish these items in accordance with the completion schedule. It is incumbent on the BUYER to ensure that any GFE is serviceable, are provided with proper FAA documentation (i.e., vendor Certificate of Compliance or 8130 tag if part is repaired), and in proper working order. No schedule/cost impacts relative to unserviceable and/or improperly documented GFE will not be attributed to the GULFSTREAM level of effort.

Additional definitions for application specific terms used in this spec are as follows:

Group A Provisions

The items, parts or components to be permanently or semi-permanently installed in an aircraft to support, secure, interconnect or accommodate specific items of equipment provided in a complementary Group B kit.

Space, Weight, Cooling, and Power

This requirement accommodates future installation of equipment. Space provisions for a specific installation shall mean that the space required for that installation is unoccupied in the aircraft.

“Space provisions” does not imply that any attaching structure, brackets, bolt holes, electrical wiring and connectors, etc., shall be furnished, designed or installed, or that the installation itself shall be accomplished. Space and weight provisions are based on the volume of generic classes of equipment, which shall allow the future installation of equipment without changes to existing structure, mounting location and other compartment features. Included in the provisions are space and weight for shock mounts, connectors, cooling air, etc. as required. Weight for items in this definition is not included in the specification weight, empty. However, the weight and location of these items shall be determined to not be detrimental to the balance and inertial characteristics of the aircraft. Power provisions require the allocation of generator and battery capacity to add future capability without changing the electrical system configuration. Cooling provisions require the allocation of sufficient cooling capacity to add future capability without changing the cooling system configuration.

Completion Center

The term Completion Center is used commercially to identify the facility at which an FAA flight

Certified, Production “Green Aircraft” undergoes interior outfitting, paint, etc. to meet specific requirements of the BUYER purchasing the completed aircraft. An aircraft undergoing “completion” therefore is being outfitted to meet BUYER requirements.

Roles and Responsibilities

GULFSTREAM Government Program Manager

The GULFSTREAM Government Program Manager assigned to interface with the BUYER during the completion process is responsible for satisfying the BUYER's requirements as outlined and defined by this document and the terms and conditions of the Contract. The Program Manager, however, cannot obligate GULFSTREAM contractually.

Customer Delivery Executive

The Customer Delivery Executive assigned to interface with the GULFSTREAM BUYER Program

Manager for the day-to-day operation during the completion process is responsible for satisfying the

GULFSTREAM BUYER Program Manager and the BUYER's directives and requirements as outlined and defined by this document and the BUYER’s approved Design Package and the terms and conditions of the Contract.

Aircraft Manager

The Aircraft Manager assigned to the aircraft has the responsibility for overseeing the completion of the aircraft in accordance with this document and the engineering documentation.

BUYER Representatives

GULFSTREAM agrees that BUYER Representatives shall have reasonable access to GULFSTREAM facilities and the aircraft while the aircraft is in the completion process. GULFSTREAM regulations concerning employees and facilities shall be observed by representatives. The BUYER

Representative shall coordinate all transactions through the assigned BUYER Program Manager.

Viewing Rights

GULFSTREAM shall not show the aircraft to prospective GULFSTREAM customers throughout the completion process without prior approval by the BUYER. Such viewing shall be done at a time that shall not affect the Completion Center work schedule and shall be under the strict supervision of a

GULFSTREAM representative.

Work Change Requests (WCRs)

Should the BUYER request changes beyond the provisions of this document, such additions, deletions and/or changes shall be accomplished by a Work Change Request (WCR) document. When such changes are proposed, equitable adjustments in the contract price, the delivery date, and the aircraft weight, if applicable, shall be made and accepted by both GULFSTREAM and the BUYER prior to initiating the work on the aircraft. GULFSTREAM initiated changes shall be submitted to the BUYER for approval.

Procedures

The procedures and inspections outlined in this document shall be adhered to during the completion of the aircraft at GULFSTREAM.

Aircraft Service Changes

Optional Aircraft Service Changes (ASCs) as identified in the G550 Product Specification for the applicable block of aircraft are available at an additional cost for incorporation on the aircraft, at the

BUYER’s request. However, prior to the installation of any additional Aircraft Service Change, GULFSTREAM shall review with the BUYER any possible impact to the delivery schedule, and mutually agree upon a time of installation. (Reference section 6000)

Customer Bulletins, Alert Customer Bulletins and Maintenance and Operations Letters

Customer Bulletins (CB’s), Alert Customer Bulletins (ACB’s) and Maintenance and Operations Letters issued prior to the completion delivery date shall be installed at no additional cost to the BUYER. Product

Improvement Aircraft Service Changes (ASCs) as identified in the GULFSTREAM G550 Product

Specification for the applicable block of aircraft are available for inclusion in the completion process at additional cost and at the BUYER’s request. However, prior to the installation of any additional Aircraft

Service Change, GULFSTREAM shall review with the BUYER any possible impact to the delivery schedule, and mutually agree upon a time of installation. New requirements levied by the FAA after agreement that impact the configuration of the aircraft shall require GULFSTREAM to notify BUYER and provide any cost or schedule impact.

Inspection Requirements

Prior to the delivery of the aircraft to the BUYER, the GULFSTREAM BUYER Program Manager and

Completion Delivery Executive shall conduct an inspection to ensure the aircraft complies with the requirements of this document, color board and the BUYER approved Design Package and the terms and conditions of the Contract.

Shop Group Leaders

A Group Leader shall be assigned from each shop to supervise the fabrication and installation of all items in accordance with this document and the BUYER-approved design package.

Quality Assurance Inspection

Incoming Inspection

An inspection of the green aircraft shall be accomplished by GULFSTREAM prior to starting any work in the Completion Center. All aircraft discrepancies documented during incoming inspection shall be corrected by GULFSTREAM at no obligation to the BUYER. A copy of all incoming inspection squawks shall be provided to the BUYER for review. The BUYER shall have the right to review all test flight squawks and attend the post flight debriefing.

Completion Inspection

Additionally, throughout the completion cycle, all avionics, electrical, interior and exterior work performed on the aircraft shall be inspected and approved by Quality Assurance personnel for conformity to all

Federal Aviation Regulations, GULFSTREAM Standards and Directives, and the BUYER-approved

Completion Specification.

Customer Inspection of Aircraft

The BUYER has requested to be notified of areas being closed. GULFSTREAM will coordinate time for inspection of these areas by BUYER reps (or DCMA case by case) with GULFSTREAM team.

Aircraft Preservation

General

After inventory and incoming inspection, the aircraft shall be prepared for modification following procedures established in accordance with GULFSTREAM Standards and Directives, and vendor/manufacturer recommendations.

Aircraft Engines

The aircraft engines and the auxiliary power unit shall be preserved in accordance with manufacturer's recommendations.

Fuel Systems

The aircraft and engine fuel systems shall be preserved per the manufacturer's instructions.

Aircraft Batteries

The batteries shall be removed, stored and reinstalled in the aircraft in accordance with the manufacturer’s recommendations.

Fire Extinguishers

The production-installed right-hand and left-hand fire extinguishers for the engines shall be disconnected during the completion program and reconnected prior to systems check.

Aircraft Tire Protection

The aircraft tires shall be properly covered to protect them from deterioration due to ultraviolet rays or ozone. The tires shall also be rotated periodically to prevent flat spots.

Weight and Balance

An estimated weight and balance document, based on the BUYER-approved Completion Specification, shall be calculated and submitted to the BUYER prior to induction of the aircraft into completion. Upon completion of the work in accordance with this document and prior to BUYER acceptance, the aircraft shall be weighed, and the actual weight and balance document, equipment list, and loading schedule shall be furnished to the BUYER. Weight and balance allowance shall be 175 lb. per person, plus 100 lb.

of baggage per person and 250 lb. galley supplies.

An as delivered aircraft Automated Weight and Balance System (AWBS) shall be provided to the BUYER.

BUYER Support Data with Maintenance Handbooks

Engineering Drawings

Upon completion of the aircraft, GULFSTREAM shall provide copies of the following engineering drawings to the BUYER in Contractor’s standard layout:

Two (2) aircraft outfitting wiring diagram manuals, including: Cockpit layout

Electronic equipment rack layout

Antenna layout

Cabin switch panel layout

Two (2) electrical load analysis supplements

Two (2) floorplans

Two (2) pitot/static system schematics (if modified)

Two (2) water system schematics

Two (2) oxygen system schematics

Two (2) Completion Center mechanical engineering diagram manuals

Cabin Operating Manual

GULFSTREAM shall provide two (2) copies of the Cabin Operating Manual that will familiarize and assist the operator with cabin systems installed at the Completion Center.

Aircraft Outfitting Systems Handbook

GULFSTREAM electronically provides the Aircraft Outfitting Systems Handbook (AOSH) to assist in training on the systems and equipment installed during outfitting. The handbook includes systems descriptions, component locations, component descriptions, system power requirements and system control and operation details where applicable.

BUYER Support Data with Maintenance Handbooks

(continued)

Photographic Documentation

GULFSTREAM reserves the right to photographically document the completion process, as well as the completed aircraft. All photographic documentation shall be accomplished at GULFSTREAM's discretion. Additionally, the BUYER shall be provided with the following items:

Four (4) 16” x 20” exterior photographs

Four (4) sets of 8” x 10” interior photographs

One (1) electronic copy of Aircraft photography

Two (2) Static Models

Cabin Familiarization Video

GULFSTREAM shall provide two (2) copies of the Cabin Familiarization Video in DVD format. The video is filmed using the BUYER’s completed aircraft and includes instructions on emergency egress and location of emergency equipment.

GULFSTREAM Equipment Removal and Functional Checks

Equipment Removal

Removal of specific equipment is required to initiate the completion program. Typical equipment removed includes but may not be limited to such items as ballast, entrance door, cockpit seats, floorboards and selected avionics equipment. Prior to submittal of the aircraft for BUYER acceptance, all removed equipment and materials required to complete the aircraft in accordance with this document shall be reinstalled and tested by GULFSTREAM at no additional expense to the BUYER.

Production-installed equipment, which shall be removed and not reinstalled in accordance with this document, shall remain the property of GULFSTREAM.

Aircraft Systems Checkout

Functional checks of the engines, auxiliary power unit, and airframe systems shall be performed on the aircraft prior to submittal of the aircraft for BUYER acceptance.

Interior

General Interior

This document defines the design, arrangement, furnishings, decorative treatment, and systems that shall be installed in the aircraft's interior. The materials and finishes specified are selected for appearance, durability, ease of maintenance and best strength-to-weight properties. The interior components are fabricated, installed, and placarded as required by the standards set forth in applicable

FAA regulations and GULFSTREAM standards and directives.

Based on current Federal Aviation Administration interpretations and policies relative to the applicable

Federal Aviation Regulations, the interior as defined herein, can be certified. Any changes to the scope of this document as required by the Federal Aviation Administration for certification, shall be evaluated by GULFSTREAM. If necessary, an equitable price adjustment shall be made to the Sales and Outfitting

Agreement.

All wood surfaces in the aircraft shall be finished in accordance with GULFSTREAM standard practices, i.e., a filled grain urethane finished straight grain walnut or equivalent.

All latches for cabinetry shall be Sealth Aero Marine (SAM) series 282 type (SAM 282-12A) unless otherwise noted in this specification and the BUYER-approved design package.

“Custom” bulkhead moldings, murals and artwork, hand-woven carpets, and exotic covering materials are not included in this specification but are available upon request at an additional charge. When finalized by the BUYER, a Work Change Request shall be executed to properly describe the BUYER’s selections and associated costs.

Due to the aging process of natural materials used in the covering of interior furnishings, a color variation may occur from the materials specified in the BUYER-approved Design Package.

GULFSTREAM assumes no liability for such color variations.

Interior

GULFSTREAM reserves the right to install equipment required under this document during the manufacturing of the production aircraft.

GULFSTREAM reserves the right to substitute components of equal or better quality in accordance with current GULFSTREAM practices and the availability of equipment or materials.

The BUYER to select Interior Finishing Design Scheme. Upon designation of Completion facility, the GULFSTREAM Principal Designer for USCG C-37B will meet with BUYER reps to review and finalize interior finish and external paint designs.

Title 14 CFR Part 91 Compliance Requirements

Compliance Basis

GULFSTREAM shall accomplish the work in accordance with the BUYER-approved Completion

Package following the standards set forth under applicable sections of Title 14 CFR Part 25 as defined by the G550 Certification Basis in Type Certificate Data Sheet (TCDS) A12EA, Title 14 CFR Part 91

Operating Regulations and GULFSTREAM Standards and Directives.

Placards and Engraving

Placards and engraving throughout the interior shall be in accordance with applicable Federal A viation Regulations. Mylar type information signs (e.g., seat locations for take-off and landing, compartment maximum weight requirements) shall be utilized.

Flammability Protection

Final assemblies/finished parts including covering materials will comply with the flammability requirements as defined in Title 14 CFR Part 25. This includes 25.853(a) for general materials;

25.853(c) for seat cushions; and 25.856(a) for thermal/acoustic materials.

Passenger Seat Certification Requirements

The passenger seat cushions shall be fabricated and certified to meet the fireblocking requirements of FAR 25.853(c) Amendment 25-83.

Passenger Briefing Cards

Twenty-five (25) passenger briefing cards shall be procured and shall be provided to the BUYER.

Covering Materials and Finish

Covering Materials

Wood veneers, solid surface, plastic laminates, paint, fabrics, leathers, and mirrors shall be used to cover interior surfaces as specified in the BUYER-approved design package. All exposed edges, moldings, and doorjambs shall be fabricated from matching fabrics, hardwoods, plastic laminates, or metal caps. Veneer protection on the corners throughout the cabin shall be installed. Materials used for interior surfaces of cabinetry and drawers shall be covered with laminate selected by GULFSTREAM and approved by the

BUYER to coordinate with the interior. The airstair, cockpit, and aft baggage material shall be standard

GULFSTREAM completion material due to certification requirements.

Metal Finish-Satin Nickel

All exposed metal trim throughout the passenger cabin interior to include the galley/galley annex and lavatories, such as seal hasps, air gaspers, reading and table light assemblies, ashtrays, cupholders, switch bezels, exposed seat hardware and galley/lavatory hardware, shall be finished in Quaker City

Plating (QCP 310) Brushed Satin Nickel in accordance with the BUYER-approved design package. Heavy wear items such as striker plates and threshold plates shall be stainless steel, brass, or equivalent.

Additional air gaspers, map/reading lights and cupholders installed in the cockpit during the completion process shall be plated with satin nickel. The seat hardware installed in the cockpit shall retain its brushed aluminum finish. The plated finish on the production installed hardware in the baggage compartment shall be retained.

Floor Covering

Floor Covering and Under-padding

Floor coverings, in accordance with the BUYER-approved design package, shall include the vestibule, forward communication area, main cabin, galley area, aft lavatory and baggage compartment floors. All carpet edges shall be sealed to prevent raveling and under-padding shall be installed. The baggage carpet shall include a flap to protect the baggage doorjamb.

A threshold plate shall be installed at the main aircraft entry door, applicable cabin areas and the external baggage entry door in accordance with the BUYER-approved design package.

The production-installed cockpit carpeting shall be gray low loop. Scuff plates shall be incorporated into the carpeting below the pilot and copilot rudder pedals.

The floor covering in the entryway, galley, aft lavatory and baggage areas shall be of Gerflor (P/N

497F4442) material.

Carpet and pad shall be commercial grade.

Spare Floor Covering

One spare set of carpet and throw rugs shall be supplied.

The spare carpet shall be cut to fit the vestibule, forward communications area, main cabin area and shall be ready for installation. All carpet edges shall be sealed to prevent raveling.

Floor Covering

Aisle Runner

Vinyl maintenance aisle runners shall be provided as loose equipment for the interior of the Aircraft

(Section 2550) and shall be for ground use only. One (1) maintenance runner shall be provided for the entry/vestibule area and the main cabin area (from fwd. cabin door to galley). The runner for the main cabin area shall cover the center of the aisle and shall be held in place with snaps and quarter- turn fasteners. The aisle runner shall not extend outboard between the seats.

Moisture Seals

Moisture seals shall be installed on the floorboards under the galley, the galley annex, the forward lavatory and the aft lavatory.

Under galley floor moisture protection. Mylar tape shall be applied to the floor directly under the galley, centerboards, and galley annex area preventing liquids from penetrating the floor.

Floor boards shall have white epoxy top coat applied to top surface prior to installation during production.

Material Soil and Stain Prevention Treatment

The interior fabrics of the aircraft shall be treated for soil and stain prevention, excluding leather, vinyl and carpet. GULFSTREAM shall provide fabric cleaning instructions to include products and manufacturers.

Underfloor Access

Non-pressurized removable floorboards throughout the interior shall be modified for inspection and maintenance purposes to ensure access to underfloor areas without removing bulkheads and major cabinet assemblies. Production-installed blowout plugs shall provide access to the oxygen cylinders.

Include access panels (blowout plugs) for underfloor communication components that require updates.

Soundproofing

The soundproofing installation shall be accomplished in accordance with the latest techniques and materials developed by GULFSTREAM. In order to ensure that the cabin obtains maximum acoustical and thermal qualities, the partial acoustical liner concept shall be used.

Corrosion Prevention Treatment

Corrosion prevention treatment is applied during production around the upper antennas, below each emergency window from the longeron to the floor line, and around the main entry door and external baggage door per GULFSTREAM standard practices. Additional corrosion prevention ASCs 136A, 137, and 138 shall be installed. All post production antennas shall have an AVDEC gasket installed.

Cabin Headliners and Passenger Service Units

This section defines the style of the headliners, passenger service units, upwash/downwash lighting, and other cabin lighting.

Headliner and Passenger Service Units with Handrails

A GULFSTREAM interior periphery shall be installed in the aircraft in accordance with the BUYER-approved design package.

Headliner

The headliner shall extend in segments from the cockpit to the auxiliary pressure bulkhead and shall be installed in a transverse configuration.

Cabin Passenger Service Units

The passenger service units shall extend along the left-hand and right-hand sides of the passenger cabin area and shall incorporate continuous upwash/downwash lighting and full-length handrails covered with wood veneer. Each unit shall contain the passenger auto-drop oxygen components, individual swivel type cold air gaspers, cabin speakers, reading/table lights and ordinance signs. Also included in the passenger service units are access panels for the emergency exit release handles.

Cabin Lighting

Reading and Table Lights

Warm white LED light assemblies shall be installed in the passenger service units for all seats and tables. An adjacent ON/OFF switch shall be provided.

Upwash Indirect Lighting

Warm white LED light assemblies shall be installed in the passenger service units to provide indirect upwash illumination of the main cabin area. Control switches for the upwash lighting shall be located in accordance with Section 2680.

Downwash Indirect Lighting

Warm white LED light assemblies shall be installed in the passenger service units to provide indirect downwash illumination of the upper sidewalls on both sides of the cabin. Control switches for the downwash lighting shall be located in accordance with Section 2680.

Cabin Lights Master Switches

Master ON/OFF switches shall be located in accordance with Section 2140 to provide combined operation of the cabin upwash/downwash lighting for night passenger boarding.

Cabin Lighting Division

The main cabin upwash/downwash lighting shall be divided between the third and fourth cabin windows to provide fore and aft cabin control.

Cabin Lighting (continued)

Flashlight - Rechargeable

In accordance with the BUYER approved Design Package one (1) production installed flashlight originally mounted in the baggage compartment shall be relocated to the lower forward face of the right-hand aft cabin bulkhead. One (1) additional flashlight shall be installed in the same area.

Cockpit Area

This section defines the finish, furnishings, and electrical systems that shall be installed in the cockpit and cockpit vestibule areas.

Cockpit Area Furnishings and Finish—Gray

Cockpit Area Finish: Gray

Specific finish colors shall be as follows:

Instrument panels..............................................................Gray

Instrumentbezels ...........................................................Gray

Center console frames .................................................Gray

Side console frames .....................................................Gray

Glareshield....................................................................Black

Glareshield extension.........................................................Black

Overhead panel...................................................................Gray

Pilot/copilot circuit breaker panels .................................Gray

All added panels ............................................................Gray

All plastic overlay panels ...............................................Gray

Pilot/copilot control columns..........................................Black

Thrust reverser knobs..........................................Satin Nickel

Throttle lever knobs ............................................Satin Nickel

Pilot/copilot control wheels ............................................Black

Engraving.......................................................................White

Pitch trim wheel .............................................................Black

Rudder/aileron trim knobs ..............................................Gray

Side console storage boxes ...........................................Gray

Cursor control devices ......................................................Black

Steering tiller.........................................................................Black

Cockpit Glareshield

The production-installed glareshield top and upper surface of the stowable extensions (bat wings) are covered with a non-reflective material.

Control Column Boots

Black control column boots shall be fabricated and installed.

Headliner

Flush handholds shall be fabricated and installed in the cockpit headliner to assist ingress and egress to/from the cockpit.

Window Trim

Window trim shall be fabricated and installed on the windshield corner posts, side windows and upper windshield closeout.

Miscellaneous Storage

The cockpit shall be equipped with sufficient storage space for flight bags and personal professional gear as well as storage for other mission essential equipment. Compartments shall be covered with material selected by GULFSTREAM. Open storage shall be provided in place of the production-installed blanking plates where practical.

Aft Bulkhead

The forward face of the left-hand and right-hand electronic equipment racks shall be covered with materials selected by GULFSTREAM.

Airworthiness Certificate and Aircraft Certification Holder

An airworthiness certificate and aircraft certification holder shall be installed in the cockpit on the left-hand side behind the pilot seat in accordance with the applicable FAA regulations.

Cockpit Vestibule Door

A cockpit vestibule door shall be fabricated and installed to serve as a divider between the cockpit vestibule area and the entryway vestibule.

Pencil Holders

Two (2) leather multi-pencil holders, one (1) each for the pilot and copilot, shall be installed in the cockpit.

An additional multi-pencil holder shall be provided for the jump seat occupant at a 45º angle on the pilot bulkhead in accordance with the design package.

Crew Seats

The production-installed crew seats shall be retained without modification.

Jump Seat

The production-installed jump seat shall be retained and stowed in the right-hand cockpit/vestibule compartment.

Rear View Mirrors

Adjustable, wide-angle mirrors shall be installed in the side windows to permit viewing of the wing control surfaces by the crew.

Cockpit Sun Visors

A wrap-around sun visor rail, manufactured by Products, with two (2) tinted clip-on type sun visors shall be installed in the cockpit just above the windshield.

Pull-Out Side Window Shades

Two (2) “pull-out” type window shades shall be installed. When in use, the shades will cover the cockpit side windows.

Cup Holders

A cup holder shall be installed on each side console for the pilot and copilot. The cupholders shall be deep enough to help prevent spillage of drinks. Cork material shall be added to the pilot and copilot cupholders to raise coffee cups as required. An additional cup holder shall be installed for the jump seat occupant.

Lighted chart holders

Transparent lighted chart holders shall be provided for the pilot and copilot. Each control wheel shall have the necessary attach mechanism to permit the chart holders to be located when required. Storage adapters shall be mounted on the side bulkhead for the chart holders.

Cockpit Footrests

Fixed, polished stainless-steel cockpit footrests shall be fabricated and installed on the lower area of the left-hand and right-hand instrument panels for the pilot and copilot.

Smoke Goggle Holders

Smoke goggle holders shall be installed in the cockpit per the BUYER-approved design package.

Maintenance CD Storage

Maintenance CD storage shall be installed in the cockpit per the BUYER-approved design package.

Headset Hooks

Three (3) headset hooks shall be installed in the cockpit area for the flight crew.

Coat Hooks

Flush mounted coat hooks shall be installed in BUYER approved locations and shall be able to support three (3) coat hangers each.

Cockpit Panel Modifications

The following panels shall be modified to accommodate the additional installation of instruments, switches, and annunciators as required and described below:

Overhead panels

Instrument panels

Circuit breaker panels

Center pedestal

Side consoles

The overhead panels, instrument panels, circuit breaker panels, center pedestal, and side consoles shall be modified in accordance with the AVIONICS section.

Cockpit Main Circuit Breaker Panels

The production-installed back-lit circuit breaker panels shall be retained. The overlays shall be replaced or modified as required to identify added circuit breakers.

Cockpit Switch Panels

Switches and annunciators added during completion shall be similar to the type used in production-installed systems.

Cockpit Area Electrical

Cockpit Lighting

The production-installed cockpit lighting system shall retain the production-installed lighting control panels and shall be modified as follows:

Jump Seat Reading Light and Switch

The production-installed reading light for the jump seat occupant shall be switchable between white and red light and the rheostat shall be relocated.

Cockpit Floodlight and Switch

The production-installed center console floodlight shall be replaced. This floodlight shall be installed in the cockpit headliner to illuminate the center console. The production-installed switch for the floodlight shall be retained.

Overhead Map Lights

Map lights shall be installed in the cockpit headliner panel above the windshields, one (1) each for the pilot and copilot and switchable between white and red light. Each map light shall be individually controlled by an ON/OFF dimmer located on the respective lighting control panel.

Cockpit/Cockpit Vestibule Dome Lights and Switch

The production-installed cockpit/cockpit vestibule dome light shall be replaced and relocated. An additional dome light shall be installed in the headliner aft of the jump seat. A single lighted switch shall be installed in the cockpit headliner panel to control both lights.

Cockpit Area Electrical

Cabin Master Switch

The production-installed cabin master switch located in the cockpit overhead panel shall allow electrical load shedding of all cabin electrical items except cabin paging, ordinance signs, and cabin emergency lighting.

Galley Master Switch(es)

The production-installed galley master switch located in the cockpit overhead panel and in the galley control panel shall allow electrical load shedding of galley appliances.

Flashlights, Rechargeable

Two (2) production-installed flashlights shall be retained in the cockpit area.

USB Power Source

USB and 60hz outlet on the cockpit sidewall – one (1) USB port shall be located in each.

Main Entryway and Vestibule Areas

This section defines the finish, furnishings, and electrical systems that shall be installed in the main entry/vestibule area.

Main Entry Door

Airstair Modification

The two (2) production-installed airstair storage compartments shall be lined with material selected by

GULFSTREAM. Additionally, the underside of the lower step section is closed out. A color coordinated non-slip covering shall be installed on the steps.

Airstair Handrails

The production-installed airstair handrails and linkage are chrome plated. An airstair handrail extension shall be provided as loose equipment. The forward handrail shall have a flag holder socket with removable flag pole.

Airstair Lighting—Hooded

The production-installed hooded lights shall be chrome-plated then re-installed in the stair risers to illuminate the steps. One (1) light is located at each step (alternating forward to aft beginning with the top step) except the bottom step which shall have one (1) floodlight to illuminate the ramp area in front of the step. An emergency floodlight is located on the forward side of the airstair. A threshold light is located on the bottom of the forward entranceway bulkhead. Airstair lighting shall be controlled by a switch at the following locations:

The vestibule switch panel

The forward external switch panel

Airstair Door Control Switch

The production installed airstair door control switch, which is located immediately forward of the main entry door behind a hinged door, shall be retained. The control switch shall be recessed and guarded to prevent inadvertent operation

International Civil Aviation Organization (ICAO) Fireproof Identification Plate

An International Civil Aviation Organization (ICAO) fireproof identification plate has been relocated to LH tail area per ASC 011.

Vestibule Area

The vestibule encompasses the approximate area from the aft cockpit vestibule bulkhead to the main cabin forward bulkhead. The materials used for the various bulkheads, closeout panels and floor covering shall be in accordance with the BUYER-approved design package.

Entranceway

The entranceway shall include an overhead bumper pad at the main entry door.

Vestibule Lighting

Two (2) flush-mounted dome lights shall be installed in the vestibule overhead to illuminate the vestibule area. A switch at the following locations shall control the vestibule dome lights:

The vestibule switch panel

The forward external switch panel

Vestibule Switch Panel

A consolidated switch panel shall be located in the header of the forward left-hand closet compartment and shall incorporate the following switches:

Vestibule dome light......................................................................... VEST DOME on/off

Airstair lights ........................................................................................ AIRSTAIR on/off

Aisle lights.......................................................................................CABIN AISLE on/off

Cabin upwash/downwash lighting master ............................. CABIN LIGHTS ON, OFF

Crew refreshment area light ...................................................................... LIGHT on/off

Window shade master ..................................................................... SHADES up/down

Entranceway Decorative Treatment

Entranceway Decorative Treatment

Special decorative treatments such as world maps, custom wood carvings, oil paintings, decorative art, and other types of logos may be incorporated in the entranceway in accordance with the BUYER- approved design package. When finalized by the BUYER, a Work Change Request shall be executed to properly describe the modifications and the associated costs.

Jeppesen Manual Storage

Jeppesen Manual Storage—Stepwell

Storage for three (3) Jeppesen manuals shall be provided in a compact storage box in the cockpit stepwell. This box shall have a carpet covered hinged lid.

Jeppesen Manual Storage—Cockpit Sidewall

Storage for Jeppesen manuals shall be provided in the sidewall storage box of both the pilot and copilot seat.

NOTE: Other Jeppesen storage (e.g. aft of the pilot seat area, forward RH crew closet) shall be omitted.

Avionics Compartments

Forward Right-hand Electronic Equipment Rack

The production-installed electronic equipment rack close-out panel located on the right-hand side of the aircraft shall be finished in accordance with the BUYER-approved design package.

Forward Left-hand Electronic Equipment Rack

The production-installed electronic equipment rack close-out panel located on the left-hand side of the aircraft shall be finished in accordance with the BUYER-approved design package.

Vestibule Acoustical Closeout

An acoustical door shall be fabricated and installed in accordance with the BUYER-approved design package to close out the airstair door during flight.

Forward Closets

Left-hand Closet

A closet shall be fabricated and installed on the left-hand side of the aircraft in accordance with the

BUYER-approved design package. Access to the closet shall be through an aisle facing hinged door.

The closet shall incorporate the following:

The customer selected carry-on KLAS Voyager system with its associated 24 port Switch wired Cat 6 to 4 ports each to 6 cabin locations (between windows phone escutcheon). Power provisioning for the KLAS Voyager

A Secure Facsimile machine

The Crisis Management System (CMS) and associated Switch and TACLANE Integrated with the AEP handsets Supporting Secure Voice Over Internet Protocol (VoSIP) Capability

Safe NSN 7110-00-919-9214 or equivalent (with external illumination provided for the unit)

Right-Hand Closet

A closet shall be fabricated and installed on the right-hand side of the aircraft immediately forward of the

CSO station in accordance with the BUYER-approved design package. The closet shall be closed out with a hinged door and incorporate the following:

Light assembly with on/off switch

Removable coat rod

Upper storage area with two (2) 115V/60Hz outlets

One (1) first aid kit

Storage for four (4) each GULFSTREAM provided telescoping umbrellas

One (1) pull out drawer in the lower section (maximum load capacity 50 lbs.)

Lower section to provide storage for two (2) 24-Channel GPS receivers (ref section 4580)

An Airborne Executive Phone Server

NOTE: Jeppesen storage shall be omitted.

Forward Crew Refreshment Compartment

A crew refreshment compartment shall be fabricated and installed in the left-hand area of the vestibule in accordance with the BUYER-approved design package. Access to the crew refreshment compartment shall be from the aisle side door and drawers. The crew refreshment compartment shall incorporate the following:

One storage compartment (above pull-out service shelf)

One (1) pull-out service shelf

One (1) ice drawer with overboard drain

Vestibule switch panel

Miscellaneous storage

Food and drink can storage

Pull-out trash compartment drawer

Note: The lower storage area is removable to provide access for maintenance.

Forward Crew Lavatory

The forward crew lavatory shall be fabricated and installed on the left-hand side of the vestibule in accordance with the BUYER-approved design package.

Storage for toilet tissue and tri-fold paper towels shall be installed in the crew lavatory in accordance with the BUYER-approved design package. Required ordinance signs, oxygen equipment, an air gasper and a trash container shall also be installed in the crew lavatory.

Lavatory Doors

The doors of the lavatory shall be installed in accordance with the BUYER-approved Design Package.

The aft door of the lavatory (forward cabin hinged door) shall incorporate a low-profile ashtray and a positive latching mechanism to indicate when the lavatory is vacant/occupied. The forward door of the lavatory shall also incorporate a positive latching mechanism to indicate when the lavatory is vacant/occupied. The aft-side of the forward lavatory door shall be covered with a 2/3 mirror.

Ashtray

An ashtray shall be installed at each entrance of the lavatory to comply with FAA regulations.

Coat Rod

A removable coat rod retained by two (2) bulkhead mounted brackets shall be installed to allow the forward crew lavatory area to be converted to a coat closet.

Towel Bar

A towel bar shall be located on the aft face of the forward bulkhead of the lavatory.

Waste Compartment Fire Extinguisher

A self-contained Walter Kidde fire extinguisher shall be installed in the waste compartment of the forward lavatory vanity. This extinguisher shall automatically operate in case of fire in the waste container.

Sink Assembly

A stowable sink assembly shall be installed outboard and above the toilet seat area. The stowable sink shall also incorporate the necessary plumbing and drain lines for the lavatory water supply system. When the sink is stowed, water shall be shut off to the sink assembly. An in-line water heater shall be installed within the forward lavatory compartment to provide the forward lavatory hot water requirements.

Electrical

A call button, a “RETURN TO SEAT” annunciator, switches for the lavatory lights, and a toilet flush switch shall be incorporated in the lavatory in accordance with the BUYER-approved design package.